Aerospace Performance Parts is pleased to offer immediate purchasing options for General Electric Company part number 1559M54G06, which you have taken interest in. This Vane Assembly Compressor Aircraf item is listed alongside the NSN 2840-01-311-4797 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 1559M54G06 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from General Electric Company under CAGE Code 07482, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 2840-01-311-4797 part number 1559M54G06 today, knowing we will support all your operational needs with care.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-311-4797 Item PartTypeName: VANE ASSEMBLY,COMPRESSOR,AIRCRAF | 2840 | 013114797 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1559M54 | 2 | 9 | D |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 1.385 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | F110-GE-100 AIRCRAFT GAS TURBINE ENGINE |
APGF | DESIGN TYPE | COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | ABHP |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
CZCJ | STAGE NUMBER | 4 |
MATT | MATERIAL | STEEL OVERALL |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F110-4,FIG 39,IND 61; 6 PER ASSEMBLY |
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